Emergency Procedures · AGK

Partial Engine Power Loss at 500ft AG

CASA Ref: CASR Part 61 MOS Schedule 3 COPA / CAKG · FAA Ref: FAA-S-ACS-6C Area IX Task A (Emergency Approach)

Scenario & Physics Summary

Immediate pitch attitude adjustment to best glide (V_BG), check fuel selector/carb heat/switches, and select landing area within 30° cone.

Interactive 3D Visual Plates & Scenario Media

Partial Engine Power Loss at 500ft AG Plate 1
Plate 1: Partial Engine Power Loss at 500ft AG
Partial Engine Power Loss at 500ft AG Plate 2
Plate 2: Partial Engine Power Loss at 500ft AG
Partial Engine Power Loss at 500ft AG Plate 3
Plate 3: Partial Engine Power Loss at 500ft AG
Partial Engine Power Loss at 500ft AG Plate 4
Plate 4: Partial Engine Power Loss at 500ft AG

Aerodynamic & Operational Physics

CASA & FAA Exam Gotcha Alert

CASA / FAA Exam Trap: The 180° turn back to the runway after engine failure below 800-1,000ft AGL is statistically the leading cause of fatal spin accidents.

Frequently Asked Questions & Exam Explanations

Why is turning back to the runway after engine failure below 1,000ft dangerous?

The steep bank required increases stall speed and sink rate, leading to stall/spin accidents before completing the turn.

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